CN209126995U - Aircraft wing universal mount - Google Patents
Aircraft wing universal mount Download PDFInfo
- Publication number
- CN209126995U CN209126995U CN201821771166.3U CN201821771166U CN209126995U CN 209126995 U CN209126995 U CN 209126995U CN 201821771166 U CN201821771166 U CN 201821771166U CN 209126995 U CN209126995 U CN 209126995U
- Authority
- CN
- China
- Prior art keywords
- lead screw
- turned
- upper plate
- bolt
- upper substrate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 239000000758 substrate Substances 0.000 claims abstract description 22
- 230000001105 regulatory effect Effects 0.000 claims abstract description 8
- 238000003780 insertion Methods 0.000 claims abstract description 4
- 230000037431 insertion Effects 0.000 claims abstract description 4
- 239000003381 stabilizer Substances 0.000 claims description 6
- 238000005457 optimization Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
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- Tires In General (AREA)
Abstract
The utility model relates to aircraft wing universal mounts, it from top to bottom include upper substrate, height regulating frame, chassis, the bolt sleeve that lead screw is turned up is set in lower plate, it is turned up in the screw rod bottom end insertion bottom tube of lead screw, upper plate one end is hinged by pivot pin with upper substrate, and the upper plate other end is bolted with upper substrate by adjusting.The height-regulating lead screw of height regulating frame is mainly used for the height adjustment of upper substrate, adjusts the adjusting that bolt is mainly used for differing tilt angles.The utility model is suitable for the aircraft wing support of different height, tilt angle, has versatility.
Description
Technical field
The utility model relates to aircraft manufacturing engineering device technique fields, in particular to aircraft wing universal mount.
Background technique
Aircraft needs to hold up aircraft wing using lifting apparatus, the support of lifting apparatus during manufacture and maintenance
Act face needs are very high with aircraft compactness, avoid aircraft wing cannot be in balance and stable state.In the assembly and dimension of aircraft
During repairing, it is also necessary to be transported through, since locating base surface is different, need replacing lifting apparatus in fuselage transhipment, come
Adapt to the aircraft wing of different height.
Utility model content
Purpose of the utility model is to solve the above problems and provide a kind of aircraft wing universal mounts, facilitate adjusting
Bearing height and adjusting support angle.
To solve the above-mentioned problems, the technical solution adopted in the utility model is as follows:
Aircraft wing universal mount, which is characterized in that from top to bottom include upper substrate 1, height regulating frame 2, chassis 3, height
It spends adjusting bracket 2 to include bottom tube 21, lower plate 22, lead screw 23, upper plate 24 is turned up, bottom tube 21 is fixedly connected with lower plate 22, and lead screw is turned up
Bolt sleeve 231 be set to lower plate 22 on, be turned up lead screw 232 bottom end of screw rod insertion bottom tube 21 in, be turned up lead screw screw rod 232 push up
Portion is fixedly connected with upper plate 24, and the screw rod 232 that lead screw is turned up is equipped with rotating ring 233, and 24 one end of upper plate and upper substrate 1 pass through axis
Pin 11 is hinged, and 24 other end of upper plate is connect with upper substrate 1 by adjusting bolt 12, adjusts 12 top of bolt and upper substrate 1 is fixed
Connection adjusts and is cased with buffer spring 13 on bolt 12, adjust bolt 12 pass through upper plate 24 bolt hole and 24 top of upper plate by
Nut is fixed.
Optimization, 23 two sides of height-regulating lead screw between upper plate 24 and lower plate 22, which are equipped with, reinforces pillar 25, reinforces covering on pillar 25
There is compressed spring 26, reinforce 25 top of pillar and connect with upper plate 24, reinforces 25 bottom end of pillar and pass through lower plate 22 and at 22 bottom of lower plate
Portion is fixed by nuts.
Optimization, chassis 3 are T shape, and each frame bottom of chassis 3 is equipped with return pulley 31, and being equipped on the inside of each return pulley 31 of chassis 3 can
Stabilizer blade 32 is turned up.
The working principle of the utility model are as follows: the height-regulating lead screw of height regulating frame is mainly used for the height adjustment of upper substrate,
Make the support it is suitable for different height.It adjusts bolt and is mainly used for the adjustings of differing tilt angles, make that it is suitable for differences to incline
The support of rake angle.
The utility model has the following beneficial effects: the utility model is suitable for the aircraft wing branch of different height, tilt angle
Support has versatility.The utility model structure is simple, and strong applicability is worth of widely use.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, in the premise not made the creative labor
Under, it is also possible to obtain other drawings based on these drawings.
Fig. 1 is the structural schematic diagram of the utility model aircraft wing universal mount；
Description of symbols: upper substrate -1, adjusts bolt -12, buffer spring -13, height regulating frame -2, bottom at pivot pin -11
Pipe -21, lower plate -22, be turned up lead screw -23, bolt sleeve -231, screw rod -232, rotating ring -233, upper plate -24, reinforce pillar -25,
Compressed spring -26, chassis -3, return pulley -31, adjustable height stabilizer blade -32.
Specific embodiment
The preferred embodiment of the utility model is described in detail with reference to the accompanying drawing, so that the advantages of the utility model
It can be easier to be readily appreciated by one skilled in the art with feature, to make the protection scope of the utility model apparent clear
Define.
As shown in Figure of description 1, the aircraft wing universal mount of the utility model includes upper substrate 1, high from top to bottom
Adjusting bracket 2, chassis 3 are spent, height regulating frame 2 includes bottom tube 21, lower plate 22, lead screw 23, upper plate 24, bottom tube 21 and lower plate 22 is turned up
It is fixedly connected, the bolt sleeve 231 that lead screw is turned up is set in lower plate 22, is turned up in 232 bottom end of the screw rod insertion bottom tube 21 of lead screw, is adjusted
232 top of screw rod of high lead screw is fixedly connected with upper plate 24, and the screw rod 232 that lead screw is turned up is equipped with rotating ring 233, upper plate 24 1
End is hinged by pivot pin 11 with upper substrate 1, and 24 other end of upper plate is connect with upper substrate 1 by adjusting bolt 12, adjusts bolt 12
Top is fixedly connected with upper substrate 1, is adjusted and is cased with buffer spring 13 on bolt 12, and the bolt hole that bolt 12 passes through upper plate 24 is adjusted
And it is fixed by nuts at the top of upper plate 24.
This specific embodiment support height is adjusted: rotation rotating ring, and rotating ring, which drives, is turned up lead screw lifting, thus upper substrate
Height is raised or reduces.The adjusting bolt of upper substrate one end is adjusted, the height of the bolt adjustment upper substrate other end is adjusted, from
And the tilt angle of upper substrate is adjusted.
In order to enhance the support degree of bracket, optimize, 23 two sides of height-regulating lead screw between upper plate 24 and lower plate 22, which are equipped with, to be added
Strong pillar 25 is reinforced being cased with compressed spring 26 on pillar 25, reinforces 25 top of pillar and connect with upper plate 24, reinforces 25 bottom end of pillar
It is fixed by nuts across lower plate 22 and in 22 bottom of lower plate.Reinforce pillar and plays reinforcement supporting role.
In order to solve the problems, such as ground injustice, optimization, chassis 3 is T shape, and each frame bottom of chassis 3 is equipped with return pulley 31, bottom
Adjustable height stabilizer blade 32 is equipped on the inside of each return pulley 31 of frame 3.Adjustable height stabilizer blade 32 used in this specific embodiment include lower margin and
Screw rod at the top of lower margin, screw rod are connected through a screw thread with T shape frame.The height of adjustable height stabilizer blade 32 is adjusted by rotary screw,
It is allowed to solve the problems, such as ground injustice.
Basic principles, main features, and advantages of the present invention has been shown and described above.Current row
The technical staff of industry is it should be appreciated that the present utility model is not limited to the above embodiments, retouching in above embodiments and description
The preference of only the utility model is stated, the utility model is not limited by above-mentioned preference, is not departing from the utility model
Under the premise of spirit and scope, the utility model can also have various changes and modifications, these changes and improvements both fall within practical
In novel claimed range.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (3)
1. aircraft wing universal mount, which is characterized in that from top to bottom include upper substrate (1), height regulating frame (2), chassis
(3), height regulating frame (2) includes bottom tube (21), lower plate (22), lead screw (23), upper plate (24), bottom tube (21) and lower plate is turned up
(22) it is fixedly connected, the bolt sleeve (231) that lead screw is turned up is set on lower plate (22), and screw rod (232) the bottom end insertion of lead screw is turned up
In bottom tube (21), it is turned up at the top of the screw rod (232) of lead screw and is fixedly connected with upper plate (24), be turned up on the screw rod (232) of lead screw and set
Have rotating ring (233), upper plate (24) one end and upper substrate (1) pass through pivot pin (11) hingedly, upper plate (24) other end and upper substrate
(1) it by adjusting bolt (12) connection, adjusts and is fixedly connected at the top of bolt (12) with upper substrate (1), adjust and covered on bolt (12)
Have buffer spring (13), adjusts bolt (12) and pass through the bolt hole of upper plate (24) and be fixed by nuts at the top of upper plate (24).
2. aircraft wing universal mount according to claim 1, which is characterized in that between upper plate (24) and lower plate (22)
Lead screw (23) two sides are turned up and are equipped with and reinforce pillar (25), reinforces being cased with compressed spring (26) on pillar (25), reinforce pillar (25)
Top is connect with upper plate (24), is reinforced pillar (25) bottom end and is passed through lower plate (22) and be fixed by nuts in lower plate (22) bottom.
3. aircraft wing universal mount according to claim 1, which is characterized in that chassis (3) is T shape, and chassis (3) is each
Frame bottom is equipped with return pulley (31), is equipped with adjustable height stabilizer blade (32) on the inside of chassis (3) each return pulley (31).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821771166.3U CN209126995U (en) | 2018-10-30 | 2018-10-30 | Aircraft wing universal mount |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821771166.3U CN209126995U (en) | 2018-10-30 | 2018-10-30 | Aircraft wing universal mount |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209126995U true CN209126995U (en) | 2019-07-19 |
Family
ID=67233357
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821771166.3U Expired - Fee Related CN209126995U (en) | 2018-10-30 | 2018-10-30 | Aircraft wing universal mount |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209126995U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116443262A (en) * | 2023-06-14 | 2023-07-18 | 陕西德鑫智能科技有限公司 | Wing bracket, wing transferring and installing method |
-
2018
- 2018-10-30 CN CN201821771166.3U patent/CN209126995U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116443262A (en) * | 2023-06-14 | 2023-07-18 | 陕西德鑫智能科技有限公司 | Wing bracket, wing transferring and installing method |
| CN116443262B (en) * | 2023-06-14 | 2023-09-08 | 陕西德鑫智能科技有限公司 | Wing bracket, wing transferring and installing method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190719 |